航天器预定时间避碰编队跟踪的CBF控制策略
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作者单位:

(1.南京理工大学紫金学院 智能控制学院,南京 210000; 2.江苏科技大学 自动化学院, 江苏 镇江 212000; 3.哈尔滨工业大学 航天学院,哈尔滨 150000)

作者简介:

任丹梅(1991—),女,讲师;周荻(1969—),男,教授,博士生导师 ;李昂(1986―),男,副教授;史晓宁(1987―),女,讲师,硕士生导师

通讯作者:

史晓宁,sxnangel886@126.com

中图分类号:

V448.2

基金项目:

江苏省高校自然科学基金(21KJB510020);南京理工大学紫金学院科研团队(ZJSRT2023003);南京理工大学紫金学院校级科研项目(2025ZRKX0401011);南京理工大学紫金学院聚智高端人才科研启动项目(2024ZK0002)


Prescribed-time collision-free formation tracking control for multiple spacecraft using control barrier functions
Author:
Affiliation:

(1.School of Intelligent Control, Nanjing University of Science and Technology Zijin College, Nanjing 210000,China; 2.School of Automation, Jiangsu University of Science and Technology, Zhenjiang 212000, Jiangsu,China ; 3.School of Astronautics, Harbin Institute of Technology, Harbin 150000,China)

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    摘要:

    为了显著提升航天器编队协同控制的响应速度,满足严格时间窗口的编队任务要求,设计一种新型预定时间保性能控制框架。该框架旨在同时应对编队系统中普遍存在的3个关键问题:航天器感知范围受限、执行机构饱和约束及编队成员间的碰撞规避。首先,结合误差转换技术与滑模控制方法,构建了控制李雅普诺夫函数条件,不仅能保障系统在预定时间内实现编队目标,同时保证了预设的瞬态响应性能和稳态精度。其次,通过引入高阶控制障碍函数,实现了对相邻航天器间相对距离的精确管控,在维持编队通信拓扑连通性的同时,有效规避了碰撞风险。进一步,采用二次规划方法求解最优控制量,在考虑执行机构饱和约束的前提下,实现了预定时间收敛、拓扑连通保持和碰撞规避的多目标协同优化。最后,通过数值仿真对所提控制框架的有效性进行了系统验证,结果表明,该方案在满足多种约束条件下具有良好的控制性能和可靠性。

    Abstract:

    To significantly enhance the response speed of spacecraft formation coordination and meet strict time-window requirements for formation missions, this paper develops a novel prescribed-time performance-guaranteed control framework. This framework effectively addresses three critical challenges prevalent in formation systems: limited perception range, actuator saturation constraints, and inter-agent collision avoidance requirements. First, by integrating error transformation technique with sliding mode control, a control Lyapunov function condition is constructed. This design not only ensures the system meets strict timing requirements for formation tasks, but also guarantees prescribed transient response characteristics and steady-state performance metrics. Second, through the establishment of high-order control barrier functions, precise regulation of relative distances between adjacent spacecraft is achieved, maintaining formation communication topology connectivity while effectively preventing collision risks. Furthermore, this study employs quadratic programming to solve for optimal control inputs, realizing multi-objective coordinated optimization of prescribed-time convergence, topology connectivity maintenance, and collision avoidance control under actuator saturation constraints. To validate the effectiveness of the proposed control framework, systematic performance verification is conducted through numerical simulations. The simulation results fully demonstrate the reliability and superiority of the proposed control scheme in satisfying all specified constraints.

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任丹梅,周荻,李昂,史晓宁.航天器预定时间避碰编队跟踪的CBF控制策略[J].哈尔滨工业大学学报,2026,58(3):110. DOI:10.11918/202505015

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  • 收稿日期:2025-05-09
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  • 在线发布日期: 2026-03-31
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